EP0551152A1 - Miniature acceleration sensor using vibrating beams in the bending mode - Google Patents

Miniature acceleration sensor using vibrating beams in the bending mode Download PDF

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Publication number
EP0551152A1
EP0551152A1 EP93200009A EP93200009A EP0551152A1 EP 0551152 A1 EP0551152 A1 EP 0551152A1 EP 93200009 A EP93200009 A EP 93200009A EP 93200009 A EP93200009 A EP 93200009A EP 0551152 A1 EP0551152 A1 EP 0551152A1
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EP
European Patent Office
Prior art keywords
sensor according
blades
accelerometric sensor
electrode
sections
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
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EP93200009A
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German (de)
French (fr)
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EP0551152B1 (en
Inventor
Denis 2 Avenue Du Berry Bt E3 Janiaud
Serge Muller
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Office National dEtudes et de Recherches Aerospatiales ONERA
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Office National dEtudes et de Recherches Aerospatiales ONERA
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/097Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by vibratory elements
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P2015/0805Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration
    • G01P2015/0822Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass
    • G01P2015/0825Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass
    • G01P2015/0828Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass the mass being of the paddle type being suspended at one of its longitudinal ends

Definitions

  • the present invention relates, in general, to a miniature accelerometric sensor which can be used for example for guiding missiles or satellites and in the automotive sector for applications such as improved braking assistance, and active suspension.
  • the invention relates to a sensor comprising a fixed solid part, a mobile solid part, two vibrating blades made of piezoelectric material working in flexion, and two articulations.
  • This sensor takes advantage of the high sensitivity of the frequency of the two blades vibrating in flexion, to compression or extension forces which are exerted longitudinally on the blades when the mobile mass part constituting the test mass of the sensor is subjected to transverse acceleration.
  • the compression of one of the blades and the extension of the other blade are converted into electrical signals which are picked up by two pairs of electrodes supported by the vibrating blades and connected to two oscillator circuits. At the output of the oscillator circuits, a signal with differential frequency is produced, the variations of which are representative of those of acceleration.
  • the body of this CA sensor is obtained by chemical machining of a piezoelectric crystal plate, such as quartz, having a uniform thickness E, and is therefore monolithic.
  • the body of the CA sensor has the general shape of a parallelepiped and includes a part solid fixed 1 secured to a BA base, a mobile solid part 2, two vibrating blades 31 and 32 and two flexible joints 41 and 42.
  • the sensor body CA has symmetry with respect to the central longitudinal axis Z'Z.
  • the blade 31 is a beam, with a small rectangular section, electrically excited by two linear electrodes 311 and 312 printed in the form of two conductive tapes extending parallel and symmetrically with respect to the longitudinal median axis of the outer edge of the blade 31 and this, over substantially half of its length contiguous to the fixed solid part 1.
  • the electrodes 311 and 312 are terminated by two conductive plates 321 and 322 connected to two first terminals of a circuit 51 oscillator by means of two conductive wires 391 and 392.
  • An identical arrangement of electrodes and plates is provided on the blade 32 and the opposite face of the fixed part 1, in relation to a second oscillator circuit 52.
  • the outputs of the two oscillator circuits 51 and 52 are connected to a differential frequency measurement device including a frequency subtraction circuit 6 and a frequency meter 7, the frequency measured (f1-f2) by the frequency meter 7 being representative of the acceleration to measure.
  • a piezoelectric plate such as the 31 plate
  • the electrical variables are coupled to the mechanical variables (constraints).
  • This piezoelectric coupling which results from the separation of the opposite polarization charges during the deformation of the blade 31, makes it possible to maintain the resonance vibration of the blade by application of an alternating electric field produced by the circuit. 51 oscillator.
  • the blade 31 thus vibrates in flexion parallel to the median plane PM of the body of the sensor which is perpendicular to the direction DS of the sensor sensitive to acceleration.
  • a weak coupling is only obtained, which then affects the resolution of the measurement of the differential frequency (f1-f2), and therefore the acceleration which is deduced therefrom.
  • these two joints consist of two beams preferably aligned in the median plane PM of the sensor and flexible according to their thickness e4 when the sensor is subjected to an acceleration in the sensitive transverse direction DS.
  • the sensor CA thus constitutes a single-axis sensor, in the sensitive direction DS perpendicular to the plane PM.
  • the bending stiffness of the joints 41 and 42 is significantly greater than that of the vibrating blades 31 and 32.
  • the cross section ⁇ 4.e4 of the articulations 41 and 42 is clearly larger than that ⁇ 3.e3 of the vibrating blades 31 and 32 so that these blades undergo practically only the only useful forces of extension and compression .
  • the blades and joints are substantially arranged in a cross between the two solid parts 1 and 2.
  • the plane median containing the longitudinal central axes Z'1Z1 and Z'2Z2 of the blades 31 and 32 is located in an oblique plane to the median plane PM of the massive parts. It thus appears in cross section of the sensor body, an offset ⁇ between the two blades which allows the sensor body to be produced by chemical machining, without however modifying the operation of the sensor thanks to the high stiffness of the joints.
  • FIGS. 2A and 2B show two rectangular cross sections equal to that E. ⁇ of the solid parts 1 and 2, and relating to a plate made of piezoelectric material from which the body of the sensor CA is obtained. These two sections correspond to the end of two successive stages of chemical machining carried out perpendicular to the large faces F1 and F2 of the material, merged with those of the massive parts 1 and 2.
  • depth machining P2 is carried out in the two series of two aforementioned wells and in front of the locations of the joints 41 and 42 on each of the faces F1 and F2 so as to obtain the body of the final sensor.
  • the present invention aims mainly to increase the piezoelectric coupling in an accelerometric sensor comprising a fixed solid part, a mobile solid part and two blades of piezoelectric material vibrating in bending, each of the blades having ends integral with the massive parts and a longitudinal side which supports first and second electrodes.
  • the senor is characterized in that a part of the length of the blade supports on the one hand, a conductive strip of the first electrode overlapping a substantially median longitudinal axis on said side, and on the other hand a lateral conductive strip of the second electrode extending near one of the longitudinal edges of said side.
  • the first electrode comprises at least one lateral strip supported by the central part of said side, extending near one of the longitudinal edges of said side and connected to the strip of first electrode which straddles the longitudinal axis and which is supported by at least one of the two quarters of length contiguous to the massive parts
  • the second electrode comprises a conductive strip supported by the central part of said side straddling the longitudinal axis and connected to at least the lateral strip of second electrode which is supported by at least one of the two quarters of length contiguous to the solid parts.
  • the electrodes can be made in a multilayer structure, supported by the side of the blade.
  • First and second electrode contact pads can be supported by one face of the fixed part and respectively connected to a strip of first electrode and to a strip of second electrode.
  • a second objective of the invention is to provide an accelerometric sensor body with two joints whose manufacturing cost is lower than that of the aforementioned known sensor, and in particular which can be machined chemically in a single step.
  • articulations of the sensor each comprise two first sections substantially parallel to the blades and respectively integral with the fixed and movable parts, and an intermediate section perpendicular to the first sections.
  • the joints are arranged on either side of the blades and are symmetrical to each other with respect to a longitudinal axis of symmetry of the sensor which is parallel to the blades so that the overall mechanical behavior of the joints in motion staircase according to the invention is similar to that of the joints of the known sensor.
  • the solid parts, the blades and the articulations preferably constitute a monolithic body machined from the same plate of piezoelectric material of uniform thickness.
  • the machining is chemical and is carried out in a single step with the same machining depth from the faces of the plate, it is provided on the one hand, that the longitudinal side of the blade supporting the electrodes is coplanar on one of the faces of the solid parts and on the other hand, that the section width of the blades taken perpendicular to said longitudinal sides of the blades is equal to the thickness of the first sections of the joints.
  • the accelerometric sensor CA ′ comprises a sensor body and associated frequency measurement means.
  • the sensor CA is assumed to be identical to the known sensor CA with regard to the fixed fixed parts 1 and mobile 2, the vibrating blades 31 and 32 and the associated frequency measurement means. .
  • the various variants described in patent application FR-A-2650895 are integrated into the present description.
  • the measuring means consist of the two oscillator circuits 51 and 52, the frequency subtraction circuit 6 and the frequency meter 7, as described above.
  • Each oscillator circuit for example the 51 circuit, has two first terminals connected respectively to two electrode contact plates 331 and 332 supported by a large face of the solid part 1.
  • the sensor body constitutes a monolithic body machined from the same plate of piezoelectric material, such as quartz, of uniform thickness E, width ⁇ and height H1 + L3 + H2.
  • the body of the sensor CA ' has the general shape of a parallelepiped which extends vertically along the direction of the height materialized by a central longitudinal axis of symmetry Z'Z. This axis Z'Z is contained in a median plane PM of the plate parallel to the faces thereof.
  • the body of the sensor CA ′ comprises the fixed solid part 1, a mobile solid part 2, two blades 31 and 32, as well as two articulations 441 and 442 according to the invention.
  • the fixed solid part 1 and the mobile solid part 2 constitute rectangular blocks arranged at the longitudinal ends of the sensor body and therefore having thickness and width equal to those E and ⁇ of the body.
  • the fixed part is intended to be integral with the structure of a machine (not shown) by means of a housing base BA and is for example fixed to the latter by gluing.
  • the two blades 31 and 32 are thin rectangular parallelepipeds integral with the two massive parts and having a horizontal rectangular cross section defined by a thickness e3 and a width ⁇ 3 taken along the width ⁇ and the thickness E of the body of the sensor CA respectively.
  • the sides of the blades 31 and 32 turned towards the outside of the body, according to the embodiment illustrated in FIG. 3, are coplanar with the large faces of the solid parts 1 and 2 of the body of the sensor CA '.
  • an offset ⁇ between the two blades 31 and 32 is provided to facilitate chemical machining and in particular to remove material between the two blades from the faces F1 and F2 of the solid parts.
  • This offset of the blades appears on either side of a plane perpendicular to the median plane PM and containing the central longitudinal axis Z'Z.
  • the two joints 441 and 442 extend between the longitudinal ends of the solid parts 1 and 2 and on each side of the set of blades 31 and 32.
  • the joints 441 and 442 are not linear, like the beams 41 and 42 according to the prior art, but have a straight staircase profile, in side view perpendicular to the plane PM. The shape and advantages of the joints will be presented later.
  • each of the blades for example the blade 31, is maintained by means of two metal electrodes 341 and 342 having opposite polarities. These electrodes are printed by photolithography on the external longitudinal side of the blade, and are not identical.
  • the first electrode 341 is composed of three conductive strips 3411, 3421 and 3431 extending longitudinally and having lengths substantially greater than L3 / 4, and substantially greater and less than L3 / 2, respectively, where L3 denotes the length of the blades 31 and 32.
  • the first strip 3411 extends along the central longitudinal axis on the external side of the blade and is extended to the plate 331 forming a contact region of the electrode 341 on the fixed part 1.
  • the other two strips 3421 and 3431 run along the longitudinal edges of the external side, substantially on the central half of the blade.
  • the bands 3411 and 3421 are connected by a double conductive bend at opposite right angles, and the ends of the bands 3421 and 3431 located towards the mobile solid part 2 are connected by a conductive U bend.
  • the second electrode 342 comprises two conductive strips 3412 and 3422 which are parallel and similar to the strips 3411 and 3421 of the first electrode.
  • the first strip 3412 extends longitudinally from the contact plate 332 on the solid part 1, mainly along the edge of the external side of the blade 31, in the extension of the strip 3431.
  • the second strip 3422 extends along the central longitudinal axis of the external side of the blade 31, between the strips 3421 and 3431, over a length substantially less than L3 / 2, and is connected to the strip 3412 by a double conductive elbow at opposite right angles.
  • the distribution of the shear stress ⁇ shown in FIG. 6A is different from the distribution of the extension-compression stress ⁇ shown in FIG. 6B, when the ends of the blade 31 are embedded in two massive parts 1 and 2.
  • the shear stress changes sign in the middle M of the blade, while the extension-compression stress along each of the longitudinal sides of the blade changes sign at the two inflection sections I1 and I2 of the blade, located approximately L3 / 4 from the ends of the blade.
  • the fibers located on the left and on the right in the end sections of the blade 31 having the approximate length L3 / 4 are subjected to compression and extension respectively, while the fibers located on the left and on the right in the central section of the blade having the approximate length L3 / 2 are subjected to extension and compression respectively.
  • the blade flexion is located on the right in Figures 6A and 6B. The blade thus oscillates on either side of the vertical when the electric field is alternating, such as that generated by the associated oscillating circuit 51 via the two electrodes.
  • the role of the piezoelectric excitation electrodes is to create components of the electric field in the plate which induce one or the other of the two constraints ⁇ and ⁇ .
  • the two electrodes 311 and 312 extend approximately at most over half L3 / 2 of the outer longitudinal edge of the blade, or according to a variant shown in FIG. 7A, two pairs of 'parallel electrodes 311 and 312 extend respectively on the two halves of the blade approximately.
  • the electric field between the electrodes half a length of the blade generates predominantly the shear stress.
  • the electrodes are arranged so that the electric fields are opposite in the two length halves of the blade and generate opposite shear stresses, as shown in Figure 6A.
  • the active excitation zone is located mainly in the central half of the blade where the central strip 3422 belonging to the second electrode 342 is framed longitudinally by the two strips 3421 and 3431 of the first electrode 341 having the same polarity which is opposite to that of the strip 3422.
  • this configuration with "three tracks” creates two opposite components of electric field according to the thickness e3 of the blade which induce respectively stresses of extension and compression, as shown in FIG. 6B.
  • the strips 3411 and 3412 connecting this three-track configuration to the contact plates 331 and 332 also generate an electric field corresponding to the directions of the extension and compression constraints in the end section L3 / 4 adjoining the fixed part 1 according to FIG. 6B, the bands 3411 and 3412 are respectively offset substantially by e3 / 2 relative to the bands 3421 and 3422.
  • the configuration with three tracks is carried out over the entire length of the blade 31 according to another variant shown in FIG. 7B.
  • the aforementioned five strips of electrodes are found and four other conductive strips are added.
  • a fourth strip of first electrode 3441 is located along the longitudinal axis of the quarter of the blade contiguous to the movable part 2.
  • a third strip of second electrode 3432 is located in the quarter of the blade contiguous to the fixed part 1 and is symmetrical with the band 3412.
  • Fourth and fifth strips of second electrode 3442 and 3452 are located symmetrically along the edges of the quarter of the blade contiguous to the mobile part 2.
  • first conductive bridges connecting between the ends of the strips 3411 to 3441 of the first electrode 341 and second connecting conductive bridges between the ends of the strips 3412 to 3452 of the second electrode 342.
  • the first and second connecting bridges intersect substantially at quarters of length L3 / 4 of the blade from the solid parts 1 and 2.
  • the first electrode 341 is located in a first implantation plane, as shown in the figure 8A, and is superimposed on the second electrode in a second implantation plane shown in FIG. 8B, through an insulating layer.
  • the conductive bridges are shown diagrammatically by doubly arrowed segments.
  • the electrode contact pads 331 and 332 on the face F1 of the fixed part are respectively connected to one end of the strip 3411 of the first electrode 341 and to the ends of the strips 3412 and 3432 of the second electrode 342, these three bands being located mainly on the quarter-length end of the blade 31 contiguous to the fixed part 1.
  • the invention thus relates, more generally, to a configuration of two electrodes "with two or three conductive strips", which extend substantially over a quarter of the length of one side of a blade, such as the strips 3411, 3412 and / or 3432, or preferably which extend substantially over the central half of the length of one side of a blade, such as strips 3422, 3421 and / or 3432.
  • the articulation 441 is preferably symmetrical relative to the axis Y'Y, contained in the plane PM and perpendicular to the axis Z'Z.
  • the articulation in staircase 441 comprises two linear sections 4411 and 4431 forming a step and a small intermediate linear section 4421 forming a step.
  • the lengths LT of the sections 4411 and 4431 are preferably equal to each other and greater than the length E-2.e4 of the intermediate section 4421.
  • the sections 4411 and 4431 have edges of width e4 substantially parallel to the blades 31 and 32. They stand perpendicular to the short sides opposite the massive parts 1 and 2 and are symmetrical with respect to the axis Y'Y.
  • the little section 4421 extends perpendicularly to the blades 31 and 32 and to the axis Y'Y as a transverse axis.
  • the section of each section is constant and rectangular.
  • the articulation width ⁇ 4 is taken along the length ⁇ of the solid parts, and is typically less than ⁇ / 3.
  • the sections e4. ⁇ 4 of the sections 4411 and 4431 are equal to each other and less than the section (L4-2.LT) . ⁇ 4 of the intermediate section 4421.
  • the thickness e4 of the sections 4411 and 4431 is taken along the thickness E of the massive parts and is typically of the order of E / 3 to E / 10.
  • the sections of the sections of the joints 441 and 442 are significantly larger than those e3. ⁇ 3 of the vibrating blades 31 and 32.
  • the sections 4411 and 4431 stand normally on two corners adjacent to the opposite faces of the solid parts 1 and 2.
  • the sections 4411 and 4431 of the articulation 441 and the corresponding sections 4412 and 4432 of l 'articulation 442 are diagonally opposite between the massive parts.
  • the staircase profile of the joints advantageously allows chemical machining in a single step to manufacture the body of the sensor CA '.
  • a single etching depth P E- ⁇ 3 is necessary and sufficient
  • the section width ⁇ 3 of the vibrating blades 31 and 32 is equal to the section thickness e4 of the joints 441 and 442.
  • the "embedding" at the ends of the vertical sections of the joints 441 and 442 are integral with the fixed part 1 on the one hand, and the test mass 2 on the other hand. These parts 1 and 2 being massive, they establish a rigid link between the recesses of the joints 441 and 442 on each of these parts.
  • a sensor CA'a comprises a fixed part la, a movable part 2a, two blades 3a1 and 3a2 and two articulations in staircase 44a1 and 44a2, as well as electrode configurations 34a1 and 34a2 with three tracks, similar to those of the CA 'sensor.
  • the CA'a sensor differs mainly by the discoid shape of the sensor body and the U-shape of the fixed part 1a.
  • This fixed part comprises a basic discoid segment 10a which forms the fixed part proper as part 1 in the sensor CA ', two thin portions 11a1 and 11a2 standing vertically at the ends of the segment 10a and situated at the height of the counter sections. lower steps 441a1 and 441a2, and two branches 12a1 and 12a2 in the form of discoid half-segments extending the thin portions and extending substantially to the end of the movable solid part 2a.
  • the sets of thin portion and branch 11a1-12a1 and 11a2-12a2 run along the articulations 44a1 and 44a2 and the movable part 2a by means of narrow longitudinal slots 13a1 and 13a et, and notches 14a1 and 14a2 are formed around the periphery circular of the sensor, at the level of the thin portions and under the branches.
  • the semi-discoid branches 12a1 and 12a2 are fixed, for example by gluing, on the base BAa of a cylindrical housing of small size, for example 0.5 cm3.
  • the thin portions 11a1 and 11a2 intermediate between the base segment and the branches, achieve mechanical decoupling between the active central part of the sensor CA'a and the branches fixed on the base, which reduces the parasitic influence of mechanical constraints of the housing.
  • electrical connections between the electrodes 34a1 and 34a2 and sealed crossings of the base of the housing are made at the fixed branches 12a1 and 12a2, by welding on metal contact pads of rectangular shape.
  • the metal areas 33a1 and 33a2 relating to one 3a1 vibrating blades are located on one 12a2 of the branches and are connected to the corresponding electrodes 34a1 and 34a2 by two metal strips 38a1 and 38a2 supported by the visible face of the base segment 10a and the thin portion 11a2.
  • the metal areas relating to the other blade 3a2 are not visible in FIG. 10 and are preferably supported by the rear face of the other branch 12a1 so as to maintain symmetry with respect to the median axis Z'Z, including in relation to electrodes and electrical connection tapes.
  • the electrodes, the connecting strips and the contact pads can be simultaneously obtained by etching a metallic layer adhering to the piezoelectric material from conventional photolithographic processes.

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Pressure Sensors (AREA)
  • Piezo-Electric Transducers For Audible Bands (AREA)

Abstract

The sensor comprises a massive stationary part (1), a massive moving part (2) and two plates made of a piezoelectric material (31;32) vibrating in bending mode, each (31) of the plates having ends integral with the massive parts, and a longitudinal side which supports first and second electrodes. In order to improve the piezoelectric coupling in the sensor, and to subject the vibrating plates principally to extension and compression strains, a quarter of the length, or preferably the central half, of the side of the plate supports longitudinal symmetrical first electrode strips (3421, 3431) and an axial second electrode strip (3422). The sensor also comprises articulations (441, 442), integral with the massive parts, which are stepped so as to chemically manufacture in a single etching stage, a wafer of piezoelectric material of uniform thickness (E), in order to obtain a monolithic body for the sensor, which is preferably symmetrical with respect to a central axis (Z'Z). <IMAGE>

Description

La présente invention concerne, de manière générale, un capteur accélérométrique miniature pouvant être utilisé par exemple pour le guidage de missiles ou de satellites et dans le secteur automobile pour des applications telles que l'assistance améliorée au freinage , et la suspension active.The present invention relates, in general, to a miniature accelerometric sensor which can be used for example for guiding missiles or satellites and in the automotive sector for applications such as improved braking assistance, and active suspension.

Plus particulièrement, l'invention a trait à un capteur comprenant une partie massive fixe, une partie massive mobile, deux lames vibrantes en matériau piézoélectrique travaillant en flexion, et deux articulations.More particularly, the invention relates to a sensor comprising a fixed solid part, a mobile solid part, two vibrating blades made of piezoelectric material working in flexion, and two articulations.

Ce capteur met à profit la grande sensibilité de la fréquence des deux lames vibrant en flexion, à des forces de compression ou d'extension qui s'exercent longitudinalement aux lames lorsque la partie massive mobile constituant la masse d'épreuve du capteur est soumise à une accélération transversale. La compression de l'une des lames et l'extension de l'autre lame sont converties sous formes de signaux électriques qui sont captés par deux paires d'électrodes supportées par les lames vibrantes et reliées à deux circuits oscillateurs. En sortie des circuits oscillateurs est produit un signal à fréquence différentielle dont les variations sont représentatives de celles de l'accélération.This sensor takes advantage of the high sensitivity of the frequency of the two blades vibrating in flexion, to compression or extension forces which are exerted longitudinally on the blades when the mobile mass part constituting the test mass of the sensor is subjected to transverse acceleration. The compression of one of the blades and the extension of the other blade are converted into electrical signals which are picked up by two pairs of electrodes supported by the vibrating blades and connected to two oscillator circuits. At the output of the oscillator circuits, a signal with differential frequency is produced, the variations of which are representative of those of acceleration.

Un tel capteur accélérométrique est décrit dans la demande de brevet français FR-A-2650895 au nom du demandeur et est représenté à la figure 1 avec des moyens de mesure de fréquence associés.Such an accelerometric sensor is described in French patent application FR-A-2650895 in the name of the applicant and is shown in Figure 1 with associated frequency measurement means.

Le corps de ce capteur CA est obtenu par usinage chimique d'une plaque de cristal piézoélectrique, tel que quartz, ayant une épaisseur uniforme E, et est donc monolithique. Selon la représentation montrée à la figure 1, le corps du capteur CA a la forme générale d'un parallélépipède et comprend une partie massive fixe 1 solidaire d'une embase BA, une partie massive mobile 2, deux lames vibrantes 3₁ et 3₂ et deux articulations flexibles 4₁ et 4₂. Le corps de capteur CA présente une symétrie par rapport à l'axe longitudinal central Z'Z.The body of this CA sensor is obtained by chemical machining of a piezoelectric crystal plate, such as quartz, having a uniform thickness E, and is therefore monolithic. According to the representation shown in Figure 1, the body of the CA sensor has the general shape of a parallelepiped and includes a part solid fixed 1 secured to a BA base, a mobile solid part 2, two vibrating blades 3₁ and 3₂ and two flexible joints 4₁ and 4₂. The sensor body CA has symmetry with respect to the central longitudinal axis Z'Z.

La lame 3₁ est une poutre, à petite section rectangulaire, excitée électriquement par deux électrodes linéaires 31₁ et 31₂ imprimées sous la forme de deux rubans conducteurs s'étendant parallèlement et symétriquement par rapport à l'axe médian longitudinal du chant externe de la lame 31 et ce, sur sensiblement la moitié de sa longueur contigüe à la partie massive fixe 1. Sur la face correspondante de la partie fixe, les électrodes 31₁ et 31₂ sont terminées par deux plaques conductrices 32₁ et 32₂ reliées à deux premières bornes d'un circuit oscillateur 5₁ au moyen de deux fils conducteurs 39₁ et 39₂. Une disposition identique d'électrodes et de plaques est prévue sur la lame 3₂ et la face opposée de la partie fixe 1, en relation avec un second circuit oscillateur 5₂.The blade 3₁ is a beam, with a small rectangular section, electrically excited by two linear electrodes 31₁ and 31₂ printed in the form of two conductive tapes extending parallel and symmetrically with respect to the longitudinal median axis of the outer edge of the blade 31 and this, over substantially half of its length contiguous to the fixed solid part 1. On the corresponding face of the fixed part, the electrodes 31₁ and 31₂ are terminated by two conductive plates 32₁ and 32₂ connected to two first terminals of a circuit 5₁ oscillator by means of two conductive wires 39₁ and 39₂. An identical arrangement of electrodes and plates is provided on the blade 3₂ and the opposite face of the fixed part 1, in relation to a second oscillator circuit 5₂.

Les sorties des deux circuits oscillateurs 5₁ et 5₂ sont reliées à un dispositif de mesure de fréquence différentielle incluant un circuit de soustraction de fréquence 6 et un fréquencemètre 7, la fréquence mesurée (f1-f2) par le fréquencemètre 7 étant représentative de l'accélération à mesurer.The outputs of the two oscillator circuits 5₁ and 5₂ are connected to a differential frequency measurement device including a frequency subtraction circuit 6 and a frequency meter 7, the frequency measured (f1-f2) by the frequency meter 7 being representative of the acceleration to measure.

Au sein d'une lame piézoélectrique, telle que la lame 3₁, les variables électriques (champ électrique) sont couplées aux variables mécaniques (contraintes). Ce couplage piézoélectrique, qui résulte de la séparation des charges de polarisation opposées lors de la déformation de la lame 3₁, permet d'entretenir la vibration de résonance de la lame par application d'un champ électrique alternatif produit par le circuit oscillateur 5₁. La lame 3₁ vibre ainsi en flexion parallèlement au plan médian PM du corps du capteur qui est perpendiculaire à la direction DS du capteur sensible à l'accélération. Selon la disposition des électrodes montrée à la figure 1, un faible couplage est seulement obtenu, ce qui affecte alors la résolution de la mesure de la fréquence différentielle (f1-f2), et donc l'accélération qui en est déduite.Within a piezoelectric plate, such as the 3₁ plate, the electrical variables (electric field) are coupled to the mechanical variables (constraints). This piezoelectric coupling, which results from the separation of the opposite polarization charges during the deformation of the blade 3₁, makes it possible to maintain the resonance vibration of the blade by application of an alternating electric field produced by the circuit. 5₁ oscillator. The blade 3₁ thus vibrates in flexion parallel to the median plane PM of the body of the sensor which is perpendicular to the direction DS of the sensor sensitive to acceleration. According to the arrangement of the electrodes shown in FIG. 1, a weak coupling is only obtained, which then affects the resolution of the measurement of the differential frequency (f1-f2), and therefore the acceleration which is deduced therefrom.

S'agissant de la conception mécanique du capteur connu CA, celle-ci présente également des inconvénients particulièrement au sujet de la forme des articulations flexibles 4₁ et 4₂.With regard to the mechanical design of the known sensor CA, this also has drawbacks, particularly with regard to the shape of the flexible joints 4₁ and 4₂.

Il est rappelé que ces deux articulations sont constituées par deux poutres de préférence alignées dans le plan médian PM du capteur et flexibles suivant leur épaisseur e4 lorsque le capteur est soumis à une accélération suivant la direction transversale sensible DS. Le capteur CA constitue ainsi un capteur mono-axe, suivant la direction sensible DS perpendiculaire au plan PM.It is recalled that these two joints consist of two beams preferably aligned in the median plane PM of the sensor and flexible according to their thickness e4 when the sensor is subjected to an acceleration in the sensitive transverse direction DS. The sensor CA thus constitutes a single-axis sensor, in the sensitive direction DS perpendicular to the plane PM.

Afin d'exploiter au maximum la sensibilité des lames vibrantes et d'assurer un bon maintien de la masse d'épreuve du capteur constituée par la partie massive mobile 2, la raideur en flexion des articulations 4₁ et 4₂ est nettement plus grande que celle des lames vibrantes 3₁ et 3₂. En d'autres termes, la section transversale λ4.e4 des articulations 4₁ et 4₂ est nettement plus grande que celle λ3.e3 des lames vibrantes 3₁ et 3₂ afin que ces lames ne subissent pratiquement que les seules forces utiles d'extension et de compression.In order to make the most of the sensitivity of the vibrating blades and to ensure good maintenance of the test mass of the sensor constituted by the mobile massive part 2, the bending stiffness of the joints 4₁ and 4₂ is significantly greater than that of the vibrating blades 3₁ and 3₂. In other words, the cross section λ4.e4 of the articulations 4₁ and 4₂ is clearly larger than that λ3.e3 of the vibrating blades 3₁ and 3₂ so that these blades undergo practically only the only useful forces of extension and compression .

Comme montré à la figure 1, les lames et articulations sont sensiblement disposées en croix entre les deux parties massives 1 et 2. Toutefois, le plan médian contenant les axes médians longitudinaux Z'₁Z₁ et Z'₂Z₂ des lames 3₁ et 3₂ est situé dans un plan oblique au plan médian PM des parties massives. Il apparaît ainsi en section transversale du corps du capteur, un décalage δ entre les deux lames qui autorise la réalisation du corps du capteur par usinage chimique, sans cependant modifier le fonctionnement du capteur grâce à la raideur élevée des articulations.As shown in Figure 1, the blades and joints are substantially arranged in a cross between the two solid parts 1 and 2. However, the plane median containing the longitudinal central axes Z'₁Z₁ and Z'₂Z₂ of the blades 3₁ and 3₂ is located in an oblique plane to the median plane PM of the massive parts. It thus appears in cross section of the sensor body, an offset δ between the two blades which allows the sensor body to be produced by chemical machining, without however modifying the operation of the sensor thanks to the high stiffness of the joints.

Les figures 2A et 2B montrent deux sections rectangulaires transversales égales à celle E.λ des parties massives 1 et 2, et relatives à une plaque en matériau piézoélectrique à partir de laquelle est obtenu le corps du capteur CA. Ces deux sections correspondent à la fin de deux étapes successives d'usinage chimique pratiqué perpendiculairement aux grandes faces F1 et F2 du matériau, confondues avec celles des parties massives 1 et 2.FIGS. 2A and 2B show two rectangular cross sections equal to that E.λ of the solid parts 1 and 2, and relating to a plate made of piezoelectric material from which the body of the sensor CA is obtained. These two sections correspond to the end of two successive stages of chemical machining carried out perpendicular to the large faces F1 and F2 of the material, merged with those of the massive parts 1 and 2.

A la première étape (figure 2A), un usinage chimique est effectué entre les emplacements des futures articulations et des futures lames afin de creuser deux séries de deux puits ayant une profondeur P1 sur les deux faces F1, F2.In the first step (FIG. 2A), chemical machining is carried out between the locations of the future joints and of the future blades in order to dig two series of two wells having a depth P1 on the two faces F1, F2.

A la seconde étape (figure 2B), un usinage de profondeur P2 est effectué dans les deux séries de deux puits précités et devant les emplacements des articulations 4₁ et 4₂ sur chacune des faces F1 et F2 de manière à obtenir le corps du capteur définitif.In the second step (FIG. 2B), depth machining P2 is carried out in the two series of two aforementioned wells and in front of the locations of the joints 4₁ and 4₂ on each of the faces F1 and F2 so as to obtain the body of the final sensor.

La profondeur d'usinage P2 de la seconde étape est égale à (E-e4)/2, où E et e4 sont les épaisseurs des parties massives 1 et 2 et des articulations 4₁ et 4₂ respectivement, et la profondeur d'usinage P1 de la première étape est telle que : P1 = E - P2 - λ3,

Figure imgb0001

où λ3 est la longueur de section transversale des lames 3₁ et 3₂ prise perpendiculairement aux faces F1 et F2.The machining depth P2 of the second step is equal to (E-e4) / 2, where E and e4 are the thicknesses of the solid parts 1 and 2 and of the joints 4₁ and 4₂ respectively, and the machining depth P1 of the first step is such that: P1 = E - P2 - λ3,
Figure imgb0001

where λ3 is the length of cross section of the blades 3₁ and 3₂ taken perpendicular to the faces F1 and F2.

Un tel usinage en deux étapes distinctes contribue au coût de fabrication relativement élevé du capteur.Such machining in two distinct stages contributes to the relatively high manufacturing cost of the sensor.

La présente invention vise principalement à augmenter le couplage piézoélectrique dans un capteur accélérométrique comprenant une partie massive fixe, une partie massive mobile et deux lames en matériau piézoélectrique vibrant en flexion, chacune des lames ayant des extrémités solidaires des parties massives et un côté longitudinal qui supporte des première et seconde électrodes.The present invention aims mainly to increase the piezoelectric coupling in an accelerometric sensor comprising a fixed solid part, a mobile solid part and two blades of piezoelectric material vibrating in bending, each of the blades having ends integral with the massive parts and a longitudinal side which supports first and second electrodes.

A cette fin, le capteur est caractérisé en ce qu'une partie de longueur de la lame supporte d'une part, une bande conductrice de la première électrode chevauchant un axe longitudinal sensiblement médian dudit côté, et d'autre part une bande conductrice latérale de la seconde électrode s'étendant à proximité de l'un des bords longitudinaux dudit côté.To this end, the sensor is characterized in that a part of the length of the blade supports on the one hand, a conductive strip of the first electrode overlapping a substantially median longitudinal axis on said side, and on the other hand a lateral conductive strip of the second electrode extending near one of the longitudinal edges of said side.

Ainsi, grâce à ces configurations à "deux ou trois pistes" ou bandes des électrodes sur chacune des lames, ces dernières sont soumises principalement à des contraintes d'extension et de compression, et non à des contraintes de cisaillement comme dans celles du capteur connu précité.La résolution de la mesure fournie par le capteur est ainsi améliorée. Ainsi, au moins l'un des deux quarts de longueur du côté de la lame contigus aux parties massives, de préférence celui contigu à la partie fixe, peut supporter ces configurations à deux ou trois pistes.Thus, thanks to these configurations with "two or three tracks" or strips of electrodes on each of the blades, the latter are mainly subjected to stresses of extension and compression, and not to shear stresses as in those of the known sensor. The resolution of the measurement supplied by the sensor is thus improved. Thus, at least one of the two quarter lengths on the side of the blade contiguous to the solid parts, preferably that contiguous to the fixed part, can support these configurations with two or three tracks.

Plus efficacement, une autre configuration de pistes analogue aux précédentes peut s'étendre sur sensiblement la moitié centrale, seule ou associée à la configuration de pistes s'étendant sur au moins l'un des deux quarts de longueur contigus aux portions massives. Dans ce dernier cas, la première électrode comprend au moins une bande latérale supportée par la partie centrale dudit côté, s'étendant à proximité de l'un des bords longitudinaux dudit côté et reliée à la bande de première électrode qui chevauche l'axe longitudinal et qui est supportée par au moins l'un des deux quarts de longueur contigus aux parties massives, et
la seconde électrode comprend une bande conductrice supportée par la partie centrale dudit côté chevauchant l'axe longitudinal et reliée à au moins la bande latérale de seconde électrode qui est supportée par au moins l'un des deux quarts de longueur contigus aux parties massives.
More effectively, another configuration of tracks similar to the previous ones can extend over substantially the central half, alone or associated with the configuration of tracks extending over at least one of the two quarters of length contiguous to the massive portions. In the latter case, the first electrode comprises at least one lateral strip supported by the central part of said side, extending near one of the longitudinal edges of said side and connected to the strip of first electrode which straddles the longitudinal axis and which is supported by at least one of the two quarters of length contiguous to the massive parts, and
the second electrode comprises a conductive strip supported by the central part of said side straddling the longitudinal axis and connected to at least the lateral strip of second electrode which is supported by at least one of the two quarters of length contiguous to the solid parts.

Pour un certain nombre de configurations d'électrodes, et en particulier pour la configuration optimale à neuf bandes, une structure monocouche peut être insuffisante. Dans ce cas, les électrodes peuvent être réalisées dans une structure multicouche, supportée par le côté de la lame.For a number of electrode configurations, and in particular for the optimal nine-band configuration, a single-layer structure may be insufficient. In this case, the electrodes can be made in a multilayer structure, supported by the side of the blade.

Des première et seconde plages de contact d'électrode peuvent être supportées par une face de la partie fixe et respectivement reliées à une bande de première électrode et à une bande de seconde électrode.First and second electrode contact pads can be supported by one face of the fixed part and respectively connected to a strip of first electrode and to a strip of second electrode.

Un second objectif de l'invention est de fournir un corps de capteur accélérométrique à deux articulations dont le coût de fabrication est plus faible que celui du capteur connu précité, et en particulier qui peut être usiné chimiquement en une seule étape.A second objective of the invention is to provide an accelerometric sensor body with two joints whose manufacturing cost is lower than that of the aforementioned known sensor, and in particular which can be machined chemically in a single step.

Pour atteindre ce second objectif, les articulations du capteur comprennent chacune deux premiers tronçons sensiblement parallèles aux lames et respectivement solidaires des parties fixe et mobile, et un tronçon intermédiaire perpendiculaire aux premiers tronçons.To achieve this second objective, articulations of the sensor each comprise two first sections substantially parallel to the blades and respectively integral with the fixed and movable parts, and an intermediate section perpendicular to the first sections.

De préférence, les articulations sont disposées de part et d'autre des lames et sont symétriques l'une de l'autre par rapport à un axe longitudinal de symétrie du capteur qui est parallèle aux lames afin que le comportement mécanique global des articulations en marche d'escalier selon l'invention soit similaire à celui des articulations du capteur connu.Preferably, the joints are arranged on either side of the blades and are symmetrical to each other with respect to a longitudinal axis of symmetry of the sensor which is parallel to the blades so that the overall mechanical behavior of the joints in motion staircase according to the invention is similar to that of the joints of the known sensor.

Comme dans le capteur connu, les parties massives, les lames et les articulations constituent de préférence un corps monolithique usiné dans une même plaque de matériau piézoélectrique d'épaisseur uniforme. Toutefois, afin que l'usinage soit chimique et soit effectué en une seule étape avec une même profondeur d'usinage à partir des faces de la plaque, il est prévu d'une part, que le côté longitudinal de lame supportant des électrodes soit coplanaire à l'une des faces des parties massives et d'autre part, que la largeur de section des lames prise perpendiculaire auxdits côtés longitudinaux des lames soit égale à l'épaisseur des premiers tronçons des articulations.As in the known sensor, the solid parts, the blades and the articulations preferably constitute a monolithic body machined from the same plate of piezoelectric material of uniform thickness. However, so that the machining is chemical and is carried out in a single step with the same machining depth from the faces of the plate, it is provided on the one hand, that the longitudinal side of the blade supporting the electrodes is coplanar on one of the faces of the solid parts and on the other hand, that the section width of the blades taken perpendicular to said longitudinal sides of the blades is equal to the thickness of the first sections of the joints.

D'autres avantages et caractéristiques de la présente invention apparaîtront plus clairement à la lecture de la description suivante de plusieurs réalisations préférées de l'invention en référence aux dessins annexés correspondants dans lesquels :

  • la figure 1 montre une vue en perspective d'un capteur accélérométrique à lames vibrant en flexion avec des moyens de mesure de fréquence associés, selon la technique antérieure;
  • les figures 2A et 2B montrent deux coupes transversales d'un capteur accélérométrique selon la technique antérieure, prises le long du plan transversal de trace II-II dans la figure 1 et correspondant respectivement à deux étapes d'usinage chimique successives;
  • la figure 3 est une vue en perspective d'un capteur accélérométrique avec des moyens de mesure de fréquence associés, selon une première réalisation préférée de l'invention;
  • la figure 4 montre une vue en perspective à plus grande échelle d'une paire d'électrodes disposées sur une lame du capteur accélérométrique selon la figure 3;
  • la figure 5 est une vue en perspective montrant les contraintes s'exerçant sur un élément de volume d'une lame en flexion;
  • les figures 6A et 6B montrent respectivement des modèles de répartition de contrainte de cisaillement et de contrainte d'extension/compression sur une lame en flexion;
  • les figures 7A et 7B montrent des répartitions surfaciques d'électrodes imprimées sur une lame, pour un couplage électro-mécanique optimal, respectivement pour une configuration "deux pistes" déduite de la technique antérieure et pour une configuration "trois pistes" selon l'invention;
  • les figures 8A et 8B sont des vues de dessus respectivement de deux électrodes superposées selon la variante de la figure 7B;
  • les figures 9A et 9B montrent deux coupes transversales du capteur accélérométrique selon l'invention, prises le long des plans transversaux de traces IXA-IXA et IXB-IXB dans la figure 3, pour expliquer l'optimisation de l'usinage chimique; et
  • la figure 10 montre une seconde réalisation préférée d'un capteur accélérométrique selon l'invention.
Other advantages and characteristics of the present invention will appear more clearly on reading the following description of several preferred embodiments of the invention with reference to the corresponding appended drawings in which:
  • FIG. 1 shows a perspective view of an accelerometric sensor with blades vibrating in bending with associated frequency measurement means, according to the prior art;
  • FIGS. 2A and 2B show two transverse sections of an accelerometric sensor according to the prior art, taken along the transverse plane of trace II-II in FIG. 1 and corresponding respectively to two successive chemical machining steps;
  • FIG. 3 is a perspective view of an accelerometric sensor with associated frequency measurement means, according to a first preferred embodiment of the invention;
  • FIG. 4 shows a perspective view on a larger scale of a pair of electrodes arranged on a blade of the accelerometric sensor according to FIG. 3;
  • Figure 5 is a perspective view showing the stresses exerted on a volume element of a bending blade;
  • FIGS. 6A and 6B respectively show models of distribution of shear stress and of extension / compression stress on a bending blade;
  • FIGS. 7A and 7B show surface distributions of electrodes printed on a blade, for optimal electro-mechanical coupling, respectively for a "two-track" configuration deduced from the prior art and for a "three-track" configuration according to the invention ;
  • FIGS. 8A and 8B are top views respectively of two superimposed electrodes according to the variant of FIG. 7B;
  • FIGS. 9A and 9B show two cross sections of the accelerometric sensor according to the invention, taken along the transverse planes of traces IXA-IXA and IXB-IXB in FIG. 3, to explain the optimization of chemical machining; and
  • FIG. 10 shows a second preferred embodiment of an accelerometric sensor according to the invention.

Dans la description ci-après d'un capteur accélérométrique CA' selon l'invention, les parties du corps du capteur CA' et celles du corps du capteur connu CA qui sont respectivement analogues, sont désignées par les mêmes repères.In the following description of an accelerometric sensor CA 'according to the invention, the parts of the body of the sensor CA' and those of the body of the known sensor CA which are respectively similar, are designated by the same references.

En référence à la figure 3, le capteur accélérométrique CA' comprend un corps de capteur et des moyens de mesure de fréquence associés.With reference to FIG. 3, the accelerometric sensor CA ′ comprises a sensor body and associated frequency measurement means.

Afin de montrer les perfectionnements apportés par l'invention, le capteur CA' est supposé être identique au capteur connu CA en ce qui concerne les parties massives fixe 1 et mobile 2, les lames vibrantes 3₁ et 3₂ et les moyens de mesure de fréquence associés. A cet égard, les diverses variantes décrites dans la demande de brevet FR-A-2650895 sont intégrées à la présente description.In order to show the improvements made by the invention, the sensor CA 'is assumed to be identical to the known sensor CA with regard to the fixed fixed parts 1 and mobile 2, the vibrating blades 3₁ and 3₂ and the associated frequency measurement means. . In this regard, the various variants described in patent application FR-A-2650895 are integrated into the present description.

Les moyens de mesure sont constitués par les deux circuits oscillateurs 5₁ et 5₂, le circuit de soustraction de fréquence 6 et le fréquencemètre 7, comme décrit précédemment. Chaque circuit oscillateur, par exemple le circuit 5₁, possède deux premières bornes reliées respectivement à deux plaques de contact d'électrode 33₁ et 33₂ supportées par une grande face de la partie massive 1.The measuring means consist of the two oscillator circuits 5₁ and 5₂, the frequency subtraction circuit 6 and the frequency meter 7, as described above. Each oscillator circuit, for example the 5₁ circuit, has two first terminals connected respectively to two electrode contact plates 33₁ and 33₂ supported by a large face of the solid part 1.

Le corps du capteur constitue un corps monolithique usiné dans une même plaque de matériau piézoélectrique, tel que quartz, d'épaisseur uniforme E, de largeur λ et de hauteur H1 + L3 + H2. Selon la réalisation illustrée à la figure 3, le corps du capteur CA' a la forme générale d'un parallélépipède qui s'étend verticalement suivant le sens de la hauteur matérialisé par un axe longitudinal central de symétrie Z'Z. Cet axe Z'Z est contenu dans un plan médian PM de la plaque parallèle aux faces de celles-ci. Le corps du capteur CA' comprend la partie massive fixe 1, une partie massive mobile 2, deux lames 3₁ et 3₂, ainsi que deux articulations 44₁ et 44₂ selon l'invention. La partie massive fixe 1 et la partie massive mobile 2 constituent des pavés parallélépipédiques disposés aux extrémités longitudinales du corps du capteur et ayant donc des épaisseur et largeur égales à celles E et λ du corps. La partie fixe est destinée à être solidaire de la structure d'un engin (non représenté) par l'intermédiaire d'une embase de boîtier BA et est par exemple fixée à cette dernière par collage.The sensor body constitutes a monolithic body machined from the same plate of piezoelectric material, such as quartz, of uniform thickness E, width λ and height H1 + L3 + H2. According to the embodiment illustrated in Figure 3, the body of the sensor CA 'has the general shape of a parallelepiped which extends vertically along the direction of the height materialized by a central longitudinal axis of symmetry Z'Z. This axis Z'Z is contained in a median plane PM of the plate parallel to the faces thereof. The body of the sensor CA ′ comprises the fixed solid part 1, a mobile solid part 2, two blades 3₁ and 3₂, as well as two articulations 44₁ and 44₂ according to the invention. The fixed solid part 1 and the mobile solid part 2 constitute rectangular blocks arranged at the longitudinal ends of the sensor body and therefore having thickness and width equal to those E and λ of the body. The fixed part is intended to be integral with the structure of a machine (not shown) by means of a housing base BA and is for example fixed to the latter by gluing.

Les deux lames 3₁ et 3₂ sont des parallélépipèdes rectangles minces solidaires des deux parties massives et ayant une section rectangulaire transversale horizontale définie par une épaisseur e3 et une largeur λ3 prises suivant la largeur λ et l'épaisseur E du corps du capteur CA respectivement.The two blades 3₁ and 3₂ are thin rectangular parallelepipeds integral with the two massive parts and having a horizontal rectangular cross section defined by a thickness e3 and a width λ3 taken along the width λ and the thickness E of the body of the sensor CA respectively.

Les côtés des lames 3₁ et 3₂ tournés vers l'extérieur du corps, selon la réalisation illustrée à la Fig. 3, sont coplanaires aux grandes faces des parties massives 1 et 2 du corps du capteur CA'.The sides of the blades 3₁ and 3₂ turned towards the outside of the body, according to the embodiment illustrated in FIG. 3, are coplanar with the large faces of the solid parts 1 and 2 of the body of the sensor CA '.

Comme dans le capteur connu CA, un décalage δ entre les deux lames 3₁ et 3₂ est prévu pour faciliter l'usinage chimique et particulièrement retirer de la matière entre les deux lames à partir des faces F1 et F2 des parties massives. Ce décalage des lames apparaît de part et d'autre d'un plan perpendiculaire au plan médian PM et contenant l'axe longitudinal central Z'Z.As in the known sensor CA, an offset δ between the two blades 3₁ and 3₂ is provided to facilitate chemical machining and in particular to remove material between the two blades from the faces F1 and F2 of the solid parts. This offset of the blades appears on either side of a plane perpendicular to the median plane PM and containing the central longitudinal axis Z'Z.

Les deux articulations 44₁ et 44₂ s'étendent entre les extrémités longitudinales des parties massives 1 et 2 et de chaque côté de l'ensemble des lames 3₁ et 3₂. Cependant, les articulations 44₁ et 44₂ ne sont pas linéaires, comme les poutres 4₁ et 4₂ selon la technique antérieure, mais présentent un profil en marche d'escalier droit, en vue de côté perpendiculaire au plan PM. La forme et les avantages des articulations seront présentés ultérieurement.The two joints 44₁ and 44₂ extend between the longitudinal ends of the solid parts 1 and 2 and on each side of the set of blades 3₁ and 3₂. However, the joints 44₁ and 44₂ are not linear, like the beams 4₁ and 4₂ according to the prior art, but have a straight staircase profile, in side view perpendicular to the plane PM. The shape and advantages of the joints will be presented later.

Selon la réalisation illustrée à la figure 3 et détaillée à la figure 4, la résonance de chacune des lames, par exemple la lame 3₁, est entretenue par l'intermédiaire de deux électrodes métalliques 34₁ et 34₂ ayant des polarités opposées. Ces électrodes sont imprimées par photolithographie sur le côté longitudinal externe de la lame, et ne sont pas identiques.According to the embodiment illustrated in Figure 3 and detailed in Figure 4, the resonance of each of the blades, for example the blade 3₁, is maintained by means of two metal electrodes 34₁ and 34₂ having opposite polarities. These electrodes are printed by photolithography on the external longitudinal side of the blade, and are not identical.

La première électrode 34₁ est composée de trois bandes conductrices 341₁, 342₁ et 343₁ s'étendant longitudinalement et ayant respectivement des longueurs sensiblement supérieure à L3/4, et sensiblement supérieure et inférieure à L3/2, où L3 dénote la longueur des lames 3₁ et 3₂. La première bande 341₁ s'étend le long de l'axe longitudinal central du côté externe de la lame et est prolongée jusqu'à la plaque 33₁ formant une région de contact de l'électrode 34₁ sur la partie fixe 1. Les deux autres bandes 342₁ et 343₁ longent les bords longitudinaux du côté externe, sensiblement sur la moitié centrale de la lame. Ainsi, les bandes 341₁ et 342₁ sont reliées par un double coude conducteur à angles droits opposés, et les extrémités des bandes 342₁ et 343₁ situées vers la partie massive mobile 2 sont reliées par un coude en U conducteur.The first electrode 34₁ is composed of three conductive strips 341₁, 342₁ and 343₁ extending longitudinally and having lengths substantially greater than L3 / 4, and substantially greater and less than L3 / 2, respectively, where L3 denotes the length of the blades 3₁ and 3₂. The first strip 341₁ extends along the central longitudinal axis on the external side of the blade and is extended to the plate 33₁ forming a contact region of the electrode 34₁ on the fixed part 1. The other two strips 342₁ and 343₁ run along the longitudinal edges of the external side, substantially on the central half of the blade. Thus, the bands 341₁ and 342₁ are connected by a double conductive bend at opposite right angles, and the ends of the bands 342₁ and 343₁ located towards the mobile solid part 2 are connected by a conductive U bend.

La seconde électrode 34₂ comprend deux bandes conductrices 341₂ et 342₂ qui sont parallèles et analogues aux bandes 341₁ et 342₁ de la première électrode. La première bande 341₂ s'étend longitudinalement à partir de la plaque de contact 33₂ sur la partie massive 1, principalement le long du bord du côté externe de la lame 3₁, dans le prolongement de la bande 343₁. La seconde bande 342₂ s'étend le long de l'axe longitudinal central du côté externe de la lame 3₁, entre les bandes 342₁ et 343₁, sur une longueur sensiblement inférieure à L3/2, et est reliée à la bande 341₂ par un double coude conducteur à angles droits opposés.The second electrode 34₂ comprises two conductive strips 341₂ and 342₂ which are parallel and similar to the strips 341₁ and 342₁ of the first electrode. The first strip 341₂ extends longitudinally from the contact plate 33₂ on the solid part 1, mainly along the edge of the external side of the blade 3₁, in the extension of the strip 343₁. The second strip 342₂ extends along the central longitudinal axis of the external side of the blade 3₁, between the strips 342₁ and 343₁, over a length substantially less than L3 / 2, and is connected to the strip 341₂ by a double conductive elbow at opposite right angles.

Les avantages de la disposition particulière des électrodes 34₁ et 34₂ sont maintenant présentés en référence aux figures 5, 6A et 6B.The advantages of the particular arrangement of the electrodes 34₁ and 34₂ are now presented with reference to FIGS. 5, 6A and 6B.

Lorsqu'une lame 3₁ est fléchie, une section S de cette lame est soumise à deux principales contraintes mécaniques, comme montré à la figure 5. Ce sont la contrainte de cisaillement τ et la contrainte d'extension-compression σ. Les fibres du matériau piézoélectrique sont en compression dans les parties concaves de la lame et en extension dans les parties convexes. L'intégration de ces deux contraintes dans la section de la lame S aboutit aux efforts connus dans le domaine de la flexion : l'effort tranchant ∫S τ.dS et le moment fléchissant ∫S σ.y.dS.When a 3₁ blade is bent, a section S of this blade is subjected to two main mechanical stresses, as shown in FIG. 5. These are the shear stress τ and the extension-compression stress σ. The fibers of the piezoelectric material are in compression in the concave parts of the blade and in extension in the convex parts. The integration of these two constraints in the section of the blade S results in the known forces in the field of bending: the shear force ∫ S τ.dS and the bending moment ∫ S σ.y.dS.

Suivant la longueur de lame 3₁, la répartition de la contrainte de cisaillement τ montrée à la figure 6A est différente de la répartition de la contrainte d'extension-compression σ montrée à la figure 6B, lorsque les extrémités de la lame 3₁ sont encastrées dans deux parties massives 1 et 2. La contrainte de cisaillement change de signe au milieu M de la lame, tandis que la contrainte d'extension-compression le long de chacun des côtés longitudinaux de la lame change de signe aux deux sections d'inflexion I1 et I2 de la lame, situées approximativement à L3/4 des extrémités de la lame. Selon la figure 6B, les fibres localisées à gauche et à droite dans les tronçons d'extrémité de la lame 3₁ ayant la longueur approximative L3/4 sont soumises à une compression et une extension respectivement, tandis que les fibres localisées à gauche et à droite dans le tronçon central de la lame ayant la longueur approximative L3/2 sont soumises à une extension et une compression respectivement. Lorsque le sens du champ électrique est inversé, la flexion de lame est située à droite dans les figures 6A et 6B. La lame oscille ainsi de part et d'autre de la verticale lorsque le champ électrique est alternatif, tel que celui généré par le circuit oscillant associé 5₁ via les deux électrodes.Depending on the length of the blade 3₁, the distribution of the shear stress τ shown in FIG. 6A is different from the distribution of the extension-compression stress σ shown in FIG. 6B, when the ends of the blade 3₁ are embedded in two massive parts 1 and 2. The shear stress changes sign in the middle M of the blade, while the extension-compression stress along each of the longitudinal sides of the blade changes sign at the two inflection sections I1 and I2 of the blade, located approximately L3 / 4 from the ends of the blade. According to FIG. 6B, the fibers located on the left and on the right in the end sections of the blade 3₁ having the approximate length L3 / 4 are subjected to compression and extension respectively, while the fibers located on the left and on the right in the central section of the blade having the approximate length L3 / 2 are subjected to extension and compression respectively. When the direction of the electric field is reversed, the blade flexion is located on the right in Figures 6A and 6B. The blade thus oscillates on either side of the vertical when the electric field is alternating, such as that generated by the associated oscillating circuit 5₁ via the two electrodes.

Le rôle des électrodes d'excitation piézoélectrique est de créer des composantes du champ électrique dans la lame qui induisent l'une ou l'autre des deux contraintes τ et σ.The role of the piezoelectric excitation electrodes is to create components of the electric field in the plate which induce one or the other of the two constraints τ and σ.

Dans le capteur connu CA montré à la figure 1, les deux électrodes 31₁ et 31₂ s'étendent approximativement au plus sur la moitié L3/2 du chant longitudinal externe de la lame, ou selon une variante montrée à la figure 7A, deux paires d'électrodes parallèles 31₁ et 31₂ s'étendent respectivement sur les deux moitiés de la lame approximativement. Dans cette configuration à "deux pistes", le champ électrique entre les électrodes d'une moitié de longueur de la lame génère de manière prépondérante la contrainte de cisaillement. Dans la figure 7A, les électrodes sont disposées afin que les champs électriques soient opposés dans les deux moitiés de longueur de la lame et génèrent des contraintes de cisaillement opposées, comme montré à la figure 6A.In the known sensor CA shown in FIG. 1, the two electrodes 31₁ and 31₂ extend approximately at most over half L3 / 2 of the outer longitudinal edge of the blade, or according to a variant shown in FIG. 7A, two pairs of 'parallel electrodes 31₁ and 31₂ extend respectively on the two halves of the blade approximately. In this "two-track" configuration, the electric field between the electrodes half a length of the blade generates predominantly the shear stress. In Figure 7A, the electrodes are arranged so that the electric fields are opposite in the two length halves of the blade and generate opposite shear stresses, as shown in Figure 6A.

Dans le capteur CA' selon l'invention, montré à la figure 3, la zone active d'excitation est située principalement dans la moitié centrale de la lame où la bande centrale 342₂ appartenant à la seconde électrode 34₂ est encadrée longitudinalement par les deux bandes 342₁ et 343₁ de la première électrode 34₁ ayant une même polarité qui est opposée à celle de la bande 342₂. Dans ces conditions, cette configuration à "trois pistes" crée deux composantes opposées de champ électrique suivant l'épaisseur e3 de la lame qui induisent respectivement des contraintes d'extension et de compression, comme montré à la figure 6B. Pour que les bandes 341₁ et 341₂ reliant cette configuration à trois pistes aux plaques de contact 33₁ et 33₂ génèrent également un champ électrique correspondant aux sens des contraintes d'extension et de compression dans le tronçon d'extrémité L3/4 jouxtant la partie fixe 1 selon la figure 6B, les bandes 341₁ et 341₂ sont respectivement décalées sensiblement de e3/2 par rapport aux bandes 342₁ et 342₂.In the CA 'sensor according to the invention, shown in FIG. 3, the active excitation zone is located mainly in the central half of the blade where the central strip 342₂ belonging to the second electrode 34₂ is framed longitudinally by the two strips 342₁ and 343₁ of the first electrode 34₁ having the same polarity which is opposite to that of the strip 342₂. Under these conditions, this configuration with "three tracks" creates two opposite components of electric field according to the thickness e3 of the blade which induce respectively stresses of extension and compression, as shown in FIG. 6B. So that the strips 341₁ and 341₂ connecting this three-track configuration to the contact plates 33₁ and 33₂ also generate an electric field corresponding to the directions of the extension and compression constraints in the end section L3 / 4 adjoining the fixed part 1 according to FIG. 6B, the bands 341₁ and 341₂ are respectively offset substantially by e3 / 2 relative to the bands 342₁ and 342₂.

Afin d'accroître l'efficacité des électrodes, la configuration à trois pistes est réalisée sur toute la longueur de la lame 3₁ selon une autre variante montrée à la figure 7B. Dans cette variante sont retrouvées les cinq bandes précitées des électrodes et sont ajoutées quatre autres bandes conductrices. Une quatrième bande de première électrode 344₁ est située le long de l'axe longitudinal du quart de la lame contigu à la partie mobile 2. Une troisième bande de seconde électrode 343₂ est située dans le quart de la lame contigu à la partie fixe 1 et est symétrique de la bande 341₂. Des quatrième et cinquième bandes de seconde électrode 344₂ et 345₂ sont situées symétriquement le long des bords du quart de la lame contigu à la partie mobile 2.In order to increase the efficiency of the electrodes, the configuration with three tracks is carried out over the entire length of the blade 3₁ according to another variant shown in FIG. 7B. In this variant, the aforementioned five strips of electrodes are found and four other conductive strips are added. A fourth strip of first electrode 344₁ is located along the longitudinal axis of the quarter of the blade contiguous to the movable part 2. A third strip of second electrode 343₂ is located in the quarter of the blade contiguous to the fixed part 1 and is symmetrical with the band 341₂. Fourth and fifth strips of second electrode 344₂ and 345₂ are located symmetrically along the edges of the quarter of the blade contiguous to the mobile part 2.

L'implantation de ces neuf bandes conductrices est réalisée en structure multicouche, c'est-à-dire par des dépôts classiques de matière conductrice et de matière isolante de manière à superposer des premiers ponts conducteurs de liaison entre les extrémités des bandes 341₁ à 344₁ de la première électrode 34₁ et des seconds ponts conducteurs de liaison entre les extrémités des bandes 341₂ à 345₂ de la seconde électrode 34₂. Les premiers et seconds ponts de liaison se croisent sensiblement aux quarts de longueur L3/4 de la lame à partir des parties massives 1 et 2. Ainsi, la première électrode 34₁ est située dans un premier plan d'implantation, comme montré à la figure 8A, et est superposée à la seconde électrode dans un second plan d'implantation montré à la figure 8B, à travers une couche isolante. Dans la figure 7B, les ponts conducteurs sont schématisés par des segments doublement fléchés.The installation of these nine conductive strips is made in a multilayer structure, that is to say by conventional deposits of conductive material and insulating material so as to superimpose first conductive bridges connecting between the ends of the strips 341₁ to 344₁ of the first electrode 34₁ and second connecting conductive bridges between the ends of the strips 341₂ to 345₂ of the second electrode 34₂. The first and second connecting bridges intersect substantially at quarters of length L3 / 4 of the blade from the solid parts 1 and 2. Thus, the first electrode 34₁ is located in a first implantation plane, as shown in the figure 8A, and is superimposed on the second electrode in a second implantation plane shown in FIG. 8B, through an insulating layer. In FIG. 7B, the conductive bridges are shown diagrammatically by doubly arrowed segments.

Toutefois, il est à noter que cette structure multicouche des électrodes est plus onéreuse que la structure monocouche montrée à la figure 4.However, it should be noted that this multilayer structure of the electrodes is more expensive than the monolayer structure shown in FIG. 4.

Les plages de contact d'électrode 33₁ et 33₂ sur la face F1 de la partie fixe sont respectivement reliées à une extrémité de la bande 341₁ de la première électrode 34₁ et à des extrémités des bandes 341₂ et 343₂ de la seconde électrode 34₂, ces trois bandes étant situées principalement sur le quart d'extrémité de longueur de la lame 3₁ contigu à la partie fixe 1.The electrode contact pads 33₁ and 33₂ on the face F1 of the fixed part are respectively connected to one end of the strip 341₁ of the first electrode 34₁ and to the ends of the strips 341₂ and 343₂ of the second electrode 34₂, these three bands being located mainly on the quarter-length end of the blade 3₁ contiguous to the fixed part 1.

L'invention concerne ainsi, d'une manière plus générale, une configuration de deux électrodes "à deux ou trois bandes conductrices", qui s'étendent sensiblement sur un quart de la longueur d'un côté d'une lame, telles que les bandes 341₁, 341₂ et/ou 343₂, ou de préférence qui s'étendent sensiblement sur la moitié centrale de la longueur d'un côté d'une lame, telles que les bandes 342₂, 342₁ et/ou 343₂.The invention thus relates, more generally, to a configuration of two electrodes "with two or three conductive strips", which extend substantially over a quarter of the length of one side of a blade, such as the strips 341₁, 341₂ and / or 343₂, or preferably which extend substantially over the central half of the length of one side of a blade, such as strips 342₂, 342₁ and / or 343₂.

L'expérience a montré que la configuration à trois pistes selon l'invention, du type de celles illustrées aux figures 4 et 7B, procure un couplage piézoélectrique entre le champ électrique et les contraintes mécaniques supérieur à celui de la configuration connue à deux pistes. Cela se traduit par un accroissement notable de la résolution et des performances du capteur.Experience has shown that the configuration at three tracks according to the invention, of the type of those illustrated in FIGS. 4 and 7B, provides a piezoelectric coupling between the electric field and the mechanical stresses greater than that of the known configuration with two tracks. This results in a significant increase in the resolution and performance of the sensor.

S'agissant de la réalisation de la configuration monocouche à trois pistes, celle-ci n'apporte aucune difficulté supplémentaire comparativement à la configuration à deux pistes, ces deux configurations étant obtenues par des procédés photolithographiques classiques mis en oeuvre notamment dans l'industrie de l'horlogerie, compte tenu des faibles dimensions des lames et notamment de leur épaisseur e3 de l'ordre de 50 µm.Regarding the realization of the three-track monolayer configuration, this does not bring any additional difficulty compared to the two-track configuration, these two configurations being obtained by conventional photolithographic processes used in particular in the industry of horology, given the small dimensions of the blades and in particular their thickness e3 of the order of 50 μm.

En se référant à nouveau à la figure 3, l'une 44₁ des articulations est décrite en détail ci-après, puisque les articulations 44₁ et 44₂ sont symétriques par rapport à l'axe central longitudinal de symétrie Z'Z du capteur CA'.Referring again to Figure 3, one 44₁ of the joints is described in detail below, since the joints 44₁ and 44₂ are symmetrical with respect to the central longitudinal axis of symmetry Z'Z of the sensor CA '.

L'articulation 44₁ est de préférence symétrique par rapport à l'axe Y'Y, contenu dans le plan PM et perpendiculaire à l'axe Z'Z. L'articulation en marche d'escalier 44₁ comporte deux tronçons linéaires 441₁ et 443₁ formant contre-marche et un petit tronçon linéaire intermédiaire 442₁ formant marche. Les longueurs LT des tronçons 441₁ et 443₁ sont de préférence égales entr'elles et supérieures à la longueur E-2.e4 du tronçon intermédiaire 442₁. Les tronçons 441₁ et 443₁ ont des chants de largeur e4 sensiblement parallèles aux lames 3₁ et 3₂. Ils se dressent perpendiculairement aux petits côtés en regard des parties massives 1 et 2 et sont symétriques par rapport à l'axe Y'Y. Le petit tronçon 442₁ s'étend perpendiculairement aux lames 3₁ et 3₂ et a l'axe Y'Y comme axe transversal. La section de chaque tronçon est constante et rectangulaire. La largeur d'articulation λ4 est prise suivant la longueur λ des parties massives, et est inférieure typiquement à λ/3. De préférence, les sections e4.λ4 des tronçons 441₁ et 443₁ sont égales entr'elles et inférieures à la section (L4-2.LT).λ4 du tronçon intermédiaire 442₁. L'épaisseur e4 des tronçons 441₁ et 443₁ est prise suivant l'épaisseur E des parties massives et est typiquement de l'ordre de E/3 à E/10. Comme selon la technique antérieure, les sections des tronçons des articulations 44₁ et 44₂ sont nettement plus grandes que celles e3.λ3 des lames vibrantes 3₁ et 3₂. Ainsi, la longueur LT des tronçons 441₁ et 443₁ est inférieure à (L3-e4)/2, en supposant L3=L4.The articulation 44₁ is preferably symmetrical relative to the axis Y'Y, contained in the plane PM and perpendicular to the axis Z'Z. The articulation in staircase 44₁ comprises two linear sections 441₁ and 443₁ forming a step and a small intermediate linear section 442₁ forming a step. The lengths LT of the sections 441₁ and 443₁ are preferably equal to each other and greater than the length E-2.e4 of the intermediate section 442₁. The sections 441₁ and 443₁ have edges of width e4 substantially parallel to the blades 3₁ and 3₂. They stand perpendicular to the short sides opposite the massive parts 1 and 2 and are symmetrical with respect to the axis Y'Y. The little section 442₁ extends perpendicularly to the blades 3₁ and 3₂ and to the axis Y'Y as a transverse axis. The section of each section is constant and rectangular. The articulation width λ4 is taken along the length λ of the solid parts, and is typically less than λ / 3. Preferably, the sections e4.λ4 of the sections 441₁ and 443₁ are equal to each other and less than the section (L4-2.LT) .λ4 of the intermediate section 442₁. The thickness e4 of the sections 441₁ and 443₁ is taken along the thickness E of the massive parts and is typically of the order of E / 3 to E / 10. As according to the prior art, the sections of the sections of the joints 44₁ and 44₂ are significantly larger than those e3.λ3 of the vibrating blades 3₁ and 3₂. Thus, the length LT of the sections 441₁ and 443₁ is less than (L3-e4) / 2, assuming L3 = L4.

Comme cela apparaît dans la figure 3, les tronçons 441₁ et 443₁ se dressent normalement sur deux coins voisins des faces en regard des parties massives 1 et 2. Les tronçons 441₁ et 443₁ de l'articulation 44₁ et les tronçons correspondants 441₂ et 443₂ de l'articulation 44₂ sont diagonalement opposés entre les parties massives.As shown in Figure 3, the sections 441₁ and 443₁ stand normally on two corners adjacent to the opposite faces of the solid parts 1 and 2. The sections 441₁ and 443₁ of the articulation 44₁ and the corresponding sections 441₂ and 443₂ of l 'articulation 44₂ are diagonally opposite between the massive parts.

Le profil en marche d'escalier des articulations autorise avantageusement l'usinage chimique en une seule étape pour fabriquer le corps du capteur CA'. Toutefois, afin qu'une seule profondeur de gravure P = E-λ3 soit nécessaire et suffisante, la largeur de section λ3 des lames vibrantes 3₁ et 3₂ est égale à l'épaisseur de section e4 des articulations 44₁ et 44₂.The staircase profile of the joints advantageously allows chemical machining in a single step to manufacture the body of the sensor CA '. However, so that a single etching depth P = E-λ3 is necessary and sufficient, the section width λ3 of the vibrating blades 3₁ and 3₂ is equal to the section thickness e4 of the joints 44₁ and 44₂.

Comme montré en coupe suivant deux plans transversaux horizontaux de part et d'autre de l'axe transversal Y'Y central au capteur CA', aux figures 9A et 9B, l'usinage chimique de profondeur P creuse notamment deux "puits" sur une largeur ((λ-δ)/2)-e3 respectivement au-dessus des tronçons de marche 442₁ et 442₂ (Fig. 9A), et deux autres "puits" sur une largeur (λ+δ) /2 respectivement au dessous des tronçons 442₁ et 442₂ (figure 9B) de manière à atteindre directement les faces des tronçons de contre-marche 443₁ et 443₂, 441₁ et 441₂, les gravures des puits de chacune des paires précitées étant réalisées à partir des faces F1 et F2 respectivement. Simultanément, au cours de gravure les contours des lames 3₁ et 3₂ sont dégagées grâce au décalage δ de celles-ci et en imposant une égalité λ3=e4 entre la largeur des lames et l'épaisseur des tronçons de contre-marche.As shown in section along two horizontal transverse planes on either side of the transverse axis Y'Y central to the sensor CA ', in FIGS. 9A and 9B, chemical machining of depth P digs in particular two "wells" on a width ((λ-δ) / 2) -e3 respectively above the walking sections 442₁ and 442₂ (Fig. 9A), and two other "wells" over a width (λ + δ) / 2 respectively below the sections 442₁ and 442₂ (Figure 9B) so as to reach directly the faces of the riser sections 443₁ and 443₂, 441₁ and 441₂, the engravings of the wells of each of the above-mentioned pairs being produced from the faces F1 and F2 respectively. Simultaneously, during etching, the contours of the blades 3₁ and 3₂ are released thanks to the offset δ of the latter and by imposing an equality λ3 = e4 between the width of the blades and the thickness of the riser sections.

Du point de vue de la fonction mécanique de l'ensemble des articulations 44₁ et 44₂ selon l'invention, celle-ci ne diffère pratiquement pas des articulations 4₁ et 4₂ du capteur connu CA.From the point of view of the mechanical function of all the 44₁ and 44₂ joints according to the invention, the latter practically does not differ from the joints 4₁ and 4₂ of the known sensor CA.

En effet, les "encastrements" aux extrémités des tronçons verticaux des articulations 44₁ et 44₂ sont solidaires de la partie fixe 1 d'une part, et de la masse d'épreuve 2 d'autre part. Ces parties 1 et 2 étant massives, elles établissent un lien rigide entre les encastrements des articulations 44₁ et 44₂ sur chacune de ces parties.Indeed, the "embedding" at the ends of the vertical sections of the joints 44₁ and 44₂ are integral with the fixed part 1 on the one hand, and the test mass 2 on the other hand. These parts 1 and 2 being massive, they establish a rigid link between the recesses of the joints 44₁ and 44₂ on each of these parts.

Le comportement mécanique de l'articulation globale 44₁ + 44₂ du capteur CA' est ainsi relativement proche de celui des poutres linéaires d'articulation 4₁ et 4₂ situées dans le plan médian PM du corps du capteur CA selon la technique antérieure, grâce aux dispositions inverses des articulations en marche d'escalier 44₁ et 44₂.The mechanical behavior of the overall articulation 44₁ + 44₂ of the sensor CA 'is thus relatively close to that of the linear beams of articulation 4₁ and 4₂ situated in the median plane PM of the body of the sensor CA according to the prior art, thanks to the reverse arrangements joints in staircase 44₁ and 44₂.

Cela ne serait pas le cas si les articulations en marche d'escalier étaient disposées dans le même sens, c'est-à-dire si l'articulation 44₂ se déduisait de l'articulation 44₁ par une translation parallèle au plan PM. En effet, il en découlerait des inconvénients lorsque le capteur est soumis à des accélérations perpendiculaires à la direction sensible DS, et en particulier à une accélération parallèle à l'axe Z'Z : la partie massive mobile 2 subirait une rotation dont l'axe serait voisin de l'axe Y'Y l'amenant dans l'un des demi-espaces situés de part et d'autre du plan PM. Ceci provoquerait une variation fréquentielle indésirable du signal de sortie délivré par le capteur, puisque celui-ci est un capteur monoaxe, c'est-à-dire ne doit être sensible qu'à la seule composante de l'accélération parallèle à DS.This would not be the case if the joints on the staircase were arranged in the same direction, that is to say if the articulation 44₂ was deduced from the articulation 44₁ by a translation parallel to the PM plan. Indeed, it would result in drawbacks when the sensor is subjected to accelerations perpendicular to the sensitive direction DS, and in particular to an acceleration parallel to the axis Z'Z: the mobile solid part 2 would undergo a rotation whose axis would be close to the Y'Y axis bringing it into one of the half-spaces located on either side of the PM plane. This would cause an undesirable frequency variation of the output signal delivered by the sensor, since the latter is a single-axis sensor, that is to say, must be sensitive only to the only component of the acceleration parallel to DS.

Pour le capteur CA' suivant l'invention, cet inconvénient n'est pas à craindre : lorsqu'une accélération est appliquée parallèlement à l'axe Z'Z, le centre de gravité de la partie massive 2 faisant office de masse d'épreuve reste situé sur l'axe Z'Z, et donc a fortiori dans le plan PM, ce qui ne provoque pas de variation du signal de sortie. Ceci est dû au fait que les articulations 44₁ et 44₂ se déduisent l'une de l'autre par une rotation de 180° autour de l'axe Z'Z. Autrement dit, elles sont symétriques l'une de l'autre par rapport à l'axe Z'Z.For the sensor CA 'according to the invention, this drawback is not to be feared: when an acceleration is applied parallel to the axis Z'Z, the center of gravity of the massive part 2 acting as test mass remains located on the axis Z'Z, and therefore a fortiori in the plane PM, which does not cause variation of the output signal. This is due to the fact that the articulations 44₁ and 44₂ are deduced from one another by a rotation of 180 ° around the axis Z'Z. In other words, they are symmetrical to each other with respect to the axis Z'Z.

Ainsi, la fonction mécanique globale des articulations 44₁ et 44₂ est semblable à celle des articulations 4₁ et 4₂ selon la technique antérieure.Thus, the overall mechanical function of the 44₁ and 44₂ joints is similar to that of the 4₁ and 4₂ joints according to the prior art.

Selon une seconde réalisation montrée à la figure 10, un capteur CA'a comporte une partie fixe la, une partie mobile 2a, deux lames 3a₁ et 3a₂ et deux articulations en marche d'escalier 44a₁ et 44a₂, ainsi que des configurations d'électrodes 34a₁ et 34a₂ à trois pistes, similaires à celles du capteur CA'.According to a second embodiment shown in FIG. 10, a sensor CA'a comprises a fixed part la, a movable part 2a, two blades 3a₁ and 3a₂ and two articulations in staircase 44a₁ and 44a₂, as well as electrode configurations 34a₁ and 34a₂ with three tracks, similar to those of the CA 'sensor.

Comparativement au capteur CA' de la figure 3, le capteur CA'a en diffère principalement par la forme discoïde du corps de capteur et par la forme en U de la partie fixe 1a.Compared to the CA 'sensor in Figure 3, the CA'a sensor differs mainly by the discoid shape of the sensor body and the U-shape of the fixed part 1a.

Cette partie fixe comporte un segment discoïde de base 10a qui forme la partie fixe proprement dite comme la partie 1 dans le capteur CA', deux portions minces 11a₁ et 11a₂ dressées verticalement aux extrémités du segment 10a et situées à la hauteur des tronçons de contre-marche inférieurs 441a₁ et 441a₂, et deux branches 12a₁ et 12a₂ en forme de demi-segments discoïdes prolongeant les portions minces et s'étendant sensiblement jusqu'à l'extrémité de la partie massive mobile 2a. Ainsi, les ensembles de portion mince et branche 11a₁-12a₁ et 11a₂-12a₂ longent les articulations 44a₁ et 44a₂ et la partie mobile 2a par l'intermédiaire de fentes longitudinales étroites 13a₁ et 13a₂, et des encoches 14a₁ et 14a₂ sont ménagées sur le pourtour circulaire du capteur, au niveau des portions minces et sous les branches.This fixed part comprises a basic discoid segment 10a which forms the fixed part proper as part 1 in the sensor CA ', two thin portions 11a₁ and 11a₂ standing vertically at the ends of the segment 10a and situated at the height of the counter sections. lower steps 441a₁ and 441a₂, and two branches 12a₁ and 12a₂ in the form of discoid half-segments extending the thin portions and extending substantially to the end of the movable solid part 2a. Thus, the sets of thin portion and branch 11a₁-12a₁ and 11a₂-12a₂ run along the articulations 44a₁ and 44a₂ and the movable part 2a by means of narrow longitudinal slots 13a₁ and 13a et, and notches 14a₁ and 14a₂ are formed around the periphery circular of the sensor, at the level of the thin portions and under the branches.

Les branches semi-discoïdes 12a₁ et 12a₂ sont fixées, par exemple par collage, sur l'embase BAa d'un boîtier cylindrique de faible encombrement, par exemple de 0,5 cm³.The semi-discoid branches 12a₁ and 12a₂ are fixed, for example by gluing, on the base BAa of a cylindrical housing of small size, for example 0.5 cm³.

Ainsi, les portions minces 11a₁ et 11a₂, intermédiaires entre le segment de base et les branches, réalisent un découplage mécanique entre la partie centrale active du capteur CA'a et les branches fixées sur l'embase, ce qui réduit l'influence parasite des contraintes mécaniques du boîtier.Thus, the thin portions 11a₁ and 11a₂, intermediate between the base segment and the branches, achieve mechanical decoupling between the active central part of the sensor CA'a and the branches fixed on the base, which reduces the parasitic influence of mechanical constraints of the housing.

Dans le même esprit, des connexions électriques entre les électrodes 34a₁ et 34a₂ et des traversées étanches de l'embase du boîtier sont réalisées au niveau des branches fixées 12a₁ et 12a₂, par soudure sur des plages de contact métalliques de forme rectangulaire. Comme illustré à la figure 10, les plages métalliques 33a₁ et 33a₂ relatives à l'une 3a₁ des lames vibrantes sont situées sur l'une 12a₂ des branches et sont reliées aux électrodes correspondantes 34a₁ et 34a₂ par deux rubans métalliques 38a₁ et 38a₂ supportés par la face visible du segment de base 10a et de la portion mince 11a₂. Les plages métalliques relatives à l'autre lame 3a₂ ne sont pas visibles dans la figure 10 et sont supportées de préférence par la face arrière de l'autre branche 12a₁ de manière à conserver la symétrie par rapport à l'axe médian Z'Z, y compris relativement aux électrodes et aux rubans de liaison électrique.In the same spirit, electrical connections between the electrodes 34a₁ and 34a₂ and sealed crossings of the base of the housing are made at the fixed branches 12a₁ and 12a₂, by welding on metal contact pads of rectangular shape. As illustrated in FIG. 10, the metal areas 33a₁ and 33a₂ relating to one 3a₁ vibrating blades are located on one 12a₂ of the branches and are connected to the corresponding electrodes 34a₁ and 34a₂ by two metal strips 38a₁ and 38a₂ supported by the visible face of the base segment 10a and the thin portion 11a₂. The metal areas relating to the other blade 3a₂ are not visible in FIG. 10 and are preferably supported by the rear face of the other branch 12a₁ so as to maintain symmetry with respect to the median axis Z'Z, including in relation to electrodes and electrical connection tapes.

Les électrodes, les rubans de liaison et les plages de contact peuvent être simultanément obtenus par gravure d'une couche métallique adhérente au matériau piézoélectrique à partir de procédés photolithographiques classiques.The electrodes, the connecting strips and the contact pads can be simultaneously obtained by etching a metallic layer adhering to the piezoelectric material from conventional photolithographic processes.

Claims (20)

Capteur accélérométrique comprenant une partie massive fixe (1), une partie massive mobile (2) et deux lames en matériau piézoélectrique vibrant en flexion (3₁; 3₂), chacune (3₁) des lames ayant des extrémités solidaires des parties massives et un côté longitudinal qui supporte des première et seconde électrodes (34₁; 34₂), caractérisé par deux articulations (44₁, 44₂) comprenant chacune deux premiers tronçons (441₁, 443₁; 441₂, 443₂) sensiblement parallèles aux lames (3₁, 3₂) et respectivement solidaires des parties fixe et mobile (1, 2), et un tronçon intermédiaire (442₁;442₂) perpendiculaire aux premiers tronçons.Accelerometric sensor comprising a fixed solid part (1), a mobile solid part (2) and two blades of piezoelectric material vibrating in bending (3₁; 3₂), each (3₁) of the blades having ends integral with the massive parts and a longitudinal side which supports first and second electrodes (34₁; 34₂), characterized by two articulations (44₁, 44₂) each comprising two first sections (441₁, 443₁; 441₂, 443₂) substantially parallel to the blades (3₁, 3₂) and respectively integral with the parts fixed and mobile (1, 2), and an intermediate section (442₁; 442₂) perpendicular to the first sections. Capteur accélérométrique conforme à la revendication 1, caractérisé en ce que les articulations (44₁, 44₂) sont disposées de part et d'autre des lames (3₁, 3₂) et sont symétriques l'une de l'autre par rapport à un axe longitudinal de symétrie (Z'Z) du capteur qui est parallèle aux lames.Accelerometric sensor according to claim 1, characterized in that the articulations (44₁, 44₂) are arranged on either side of the blades (3₁, 3₂) and are symmetrical to each other with respect to a longitudinal axis symmetry (Z'Z) of the sensor which is parallel to the blades. Capteur accélérométrique conforme à la revendication 1 ou 2, caractérisé par des longueurs (LT) des premiers tronçons (441₁, 443₁; 441₂, 443₂) qui sont égales entr'elles et supérieures à la longueur du tronçon intermédiaire (442₁; 442₂).Accelerometric sensor according to claim 1 or 2, characterized by lengths (LT) of the first sections (441₁, 443₁; 441₂, 443₂) which are equal to one another and greater than the length of the intermediate section (442₁; 442₂). Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 3, caractérisé par des sections (e4.14) des premiers tronçons (441₁, 443₁; 441₂, 443₂) qui sont égales entr'elles et inférieures à la section ((L4-2.LT).λ4) du tronçon intermédiaire (442₁; 442₂).Accelerometric sensor according to any one of claims 1 to 3, characterized by sections (e4.14) of the first sections (441₁, 443₁; 441₂, 443₂) which are equal to one another and less than the section ((L4- 2.LT) .λ4) of the intermediate section (442₁; 442₂). Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 4, caractérisé par des sections des tronçons (441₁, 442₁, 443₁; 441₂, 442₂, 443₂) des articulations (44₁; 44₂) supérieures à la section (e3.13) des lames (3₁; 3₂).Accelerometric sensor according to any one of claims 1 to 4, characterized by sections of the sections (441₁, 442₁, 443₁; 441₂, 442₂, 443₂) of the joints (44₁; 44₂) greater than the section (e3.13) of the blades (3₁; 3₂). Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 5, caractérisé par des faces des deux premiers tronçons de chacune des articulations (441₁, 443₁; 441₂, 443₂) respectivement coplanaires à des faces opposées des parties massives fixe et mobile (1, 2).Accelerometric sensor according to any one of claims 1 to 5, characterized by the faces of the first two sections of each of the articulations (441₁, 443₁; 441₂, 443₂) respectively coplanar with opposite faces of the fixed and mobile solid parts (1, 2). Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 6, caractérisé en ce que ledit côté longitudinal de lame supportant les électrodes (34₁, 34₂) est coplanaire à l'une (F1) des faces de la partie fixe (1).Accelerometric sensor according to any one of Claims 1 to 6, characterized in that the said longitudinal side of the blade supporting the electrodes (34₁, 34₂) is coplanar with one (F1) of the faces of the fixed part (1). Capteur accélérométrique conforme à la revendication 7, caractérisé par une largeur de section (13) des lames (3₁, 3₂) prise perpendiculaire auxdits côtés longitudinaux des lames, égale à l'épaisseur (e4) des premiers tronçons (441₁, 443₁; 441₂, 443₂) des articulations.Accelerometric sensor according to claim 7, characterized by a section width (13) of the blades (3₁, 3₂) taken perpendicular to said longitudinal sides of the blades, equal to the thickness (e4) of the first sections (441₁, 443₁; 441₂, 443₂) of the joints. Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 8, caractérisé en ce qu'une partie de longueur de la lame (3₁) supporte d'une part une bande conductrice (341₁; 342₂; 344₁) de la première électrode (34₁; 34₂) chevauchant un axe longitudinal sensiblement médian dudit côté, et d'autre part une bande conductrice latérale (341₂ ou 343₂; 343₁ ou 342₁; 344₂ ou 345₂) de la seconde électrode (34₂; 34₁) s'étendant à proximité de l'un des bords longitudinaux dudit côté.Accelerometric sensor according to any one of Claims 1 to 8, characterized in that a part of the length of the blade (3₁) supports on the one hand a conductive strip (341₁; 342₂; 344₁) of the first electrode (34₁ ; 34₂) overlapping a substantially median longitudinal axis on said side, and on the other share a lateral conductive strip (341₂ or 343₂; 343₁ or 342₁; 344₂ or 345₂) of the second electrode (34₂; 34₁) extending near one of the longitudinal edges of said side. Capteur accélérométrique conforme à la revendication 9, caractérisé en ce que la partie de longueur de la lame (3₁) supporte une deuxième bande conductrice latérale (343₂ ou 341₂; 342₁ ou 343₁; 345₂ ou 344₂) s'étendant symétriquement à la première bande latérale par rapport à l'axe longitudinal médian dudit côté et appartenant à la seconde électrode.Accelerometric sensor according to claim 9, characterized in that the length part of the blade (3₁) supports a second lateral conductive strip (343₂ or 341₂; 342₁ or 343₁; 345₂ or 344₂) extending symmetrically to the first lateral strip relative to the median longitudinal axis of said side and belonging to the second electrode. Capteur accélérométrique conforme à la revendication 9 ou 10, caractérisé en ce que la partie de longueur de la lame (3₁) comprend au moins l'un des deux quarts (L3/4) de longueur contigus aux parties massives (1,2).Accelerometric sensor according to claim 9 or 10, characterized in that the length part of the blade (3₁) comprises at least one of the two quarters (L3 / 4) of length contiguous to the solid parts (1,2). Capteur accélérométrique conforme à la revendication 9 ou 10, caractérisé en ce que la partie de longueur de la lame (3₁) comprend sensiblement la moitié centrale (L3/2).Accelerometric sensor according to claim 9 or 10, characterized in that the length part of the blade (3₁) comprises substantially the central half (L3 / 2). Capteur accélérométrique conforme à la revendication 11, caractérisé en ce que la première électrode (34₁) comprend au moins une bande latérale (342₁, 343₁) supportée par la partie centrale dudit côté, s'étendant à proximité de l'un des bords longitudinaux dudit côté et reliée à la bande de première électrode (341₁, 344₁) qui chevauche l'axe longitudinal et qui est supportée par au moins l'un des deux quarts de longueur contigus aux parties massives, et la seconde électrode comprend une bande conductrice (342₂) supportée par la partie centrale dudit côté chevauchant l'axe longitudinal et reliée à au moins la bande latérale de seconde électrode (341₂ ou 343₂; 344₂ ou 345₂) qui est supportée par au moins l'un des deux quarts de longueur contigus aux parties massives.Accelerometric sensor according to claim 11, characterized in that the first electrode (34₁) comprises at least one side strip (342₁, 343₁) supported by the central part of said side, extending near one of the longitudinal edges of said side and connected to the strip of first electrode (341₁, 344₁) which straddles the longitudinal axis and which is supported by at least one of the two quarter lengths contiguous to the solid parts, and the second electrode comprises a conductive strip (342₂) supported by the central part of said side straddling the longitudinal axis and connected to at least the side strip of second electrode (341₂ or 343₂; 344₂ or 345₂) which is supported by at least one of the two contiguous quarter lengths massive parts. Capteur accélérométrique conforme à l'une quelconque des revendications 9 à 13, caractérisé en ce que les électrodes (34₁, 34₂) sont sur des couches superposées d'une structure multicouche supportée par ledit côté de la lame.Accelerometric sensor according to any one of claims 9 to 13, characterized in that the electrodes (34₁, 34₂) are on superimposed layers of a multilayer structure supported by said side of the blade. Capteur accélérométrique conforme à l'une quelconque des revendications 9 à 14, caractérisé en ce que chaque électrode a une bande conductrice reliée à une plage de contact d'électrodes (33₁, 33₂) supportée par une face (F1) de la partie fixe (1).Accelerometric sensor according to any one of Claims 9 to 14, characterized in that each electrode has a conductive strip connected to an electrode contact pad (33₁, 33₂) supported by a face (F1) of the fixed part ( 1). Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 15, caractérisé en ce que les parties massives (1, 2), les lames (3₁, 3₂) et les articulations (44₁, 44₂) constituent un corps monolithique usiné dans une même plaque de matériau piézoélectrique d'épaisseur uniforme (E).Accelerometric sensor according to any one of claims 1 to 15, characterized in that the solid parts (1, 2), the blades (3₁, 3₂) and the joints (44₁, 44₂) constitute a monolithic body machined in the same plate of piezoelectric material of uniform thickness (E). Capteur accélérométrique conforme aux revendications 8 et 16, caractérisé en ce que l'usinage du corps est chimique et est effectué en une seule étape avec une même profondeur d'usinage (P) à partir des faces (F1, F2) de ladite plaque.Accelerometric sensor according to claims 8 and 16, characterized in that the machining of the body is chemical and is carried out in a single step with the same machining depth (P) from the faces (F1, F2) of said plate. Capteur accélérométrique conforme à l'une quelconque des revendications 1 à 17, caractérisé en ce que la partie fixe (la) comprend deux ensembles composés chacun d'une branche (12a₁; 12a₂) pour fixer le capteur sur une embase (BAa), et d'une portion mince (11a₁; 11a₂) reliant ladite branche à une base (10a) de la partie fixe qui est solidaire des lames (3a₁, 3a₂) et des articulations (44a₁, 44a₂) pour découpler mécaniquement la branche et la base.Accelerometric sensor according to any one of claims 1 to 17, characterized in that the fixed part (la) comprises two assemblies each composed of a branch (12a₁; 12a₂) for fixing the sensor on a base (BAa), and a thin portion (11a₁; 11a₂) connecting said branch to a base (10a) of the fixed part which is integral with the blades (3a₁, 3a₂) and the joints (44a₁, 44a₂ ) to mechanically decouple the branch and the base. Capteur accélérométrique conforme à la revendication 18, caractérisé en ce que les ensembles à branche et portion mince (12a₁, 11a₁; 12a₂, 11a₂) sont séparés des articulations (44a₁; 44a₂) et de la partie mobile (2a) par des fentes longitudinales (13a₁, 13a₂).Accelerometric sensor according to claim 18, characterized in that the branch and thin portion assemblies (12a₁, 11a₁; 12a₂, 11a₂) are separated from the articulations (44a₁; 44a₂) and the movable part (2a) by longitudinal slots ( 13a₁, 13a₂). Capteur accélérométrique conforme à la revendication 18 ou 19, caractérisé par des paires de plages de contact (33a₁, 33a₂) disposées respectivement sur les faces opposées des branches (12a₁, 12a₂) et reliées aux paires d'électrodes (34a₁, 34a₂) des lames (3a₁, 3a₂) par des paires de rubans conducteurs (38a₁, 38a₂) supportées par les portions minces (11a₁; 11a₂) et la base (10a).Accelerometric sensor according to claim 18 or 19, characterized by pairs of contact pads (33a₁, 33a₂) disposed respectively on the opposite faces of the arms (12a₁, 12a₂) and connected to the pairs of electrodes (34a₁, 34a₂) of the blades (3a₁, 3a₂) by pairs of conductive tapes (38a₁, 38a₂) supported by the thin portions (11a₁; 11a₂) and the base (10a).
EP93200009A 1992-01-06 1993-01-05 Miniature acceleration sensor using vibrating beams in the bending mode Expired - Lifetime EP0551152B1 (en)

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FR9200044A FR2685964B1 (en) 1992-01-06 1992-01-06 MINIATURE ACCELEROMETRIC SENSOR WITH BENDING VIBRATING BLADES.
FR9200044 1992-01-11

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FR2685964A1 (en) 1993-07-09
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EP0551152B1 (en) 1995-08-16
DE69300367D1 (en) 1995-09-21

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